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A numerical study of blade thickness and camber effects on vertical axis wind turbines

机译:垂直轴风力发电机叶片厚度和外倾角影响的数值研究

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摘要

This article presents the results of a two-dimensional computational study into the effects of rotor blade thickness and camber on the performance of a 5 kW scale vertical axis wind turbine. Validation is provided by reference to experimental data for a pitching aerofoil with dynamic stall phenomenon. The performance of the turbine is mapped out for a variety of different tip speed ratios and detailed investigations are presented to determine how and, most importantly, why the turbine performance varies with thickness and camber as it does. The rotor blades chosen were the NACA0012, NACA0022, NACA5522 and LS0421. The turbine rotor has a diameter of d = 3.1 m with a blade chord length of c = 0.18 m. Over the range of tip speed ratios examined, the NACA0012 profile performed with the highest overall performance of 50% at λ = 3.5. Slightly cambered aerofoils (such as the LS042I) can improve the overall performance of the vertical axis wind turbine, whereas a camber of 5% (NACA5522) results in unfavourable performance. Of the cambered blades tested, the LS0421 performs the best with maximum CP of 0.40 at λ= 3.5. A camber along the blade path causes the blades to generate higher values of torque in both the upwind and the downwind regions. It was also determined that inverted cambered profiles produce power mostly in the upwind region.
机译:本文介绍了二维计算研究的结果,研究了转子叶片厚度和外倾角对5 kW比例垂直轴风力发电机性能的影响。通过参考具有动态失速现象的俯仰翼型的实验数据来提供验证。针对各种不同的叶尖速比绘制了涡轮机的性能,并进行了详细研究,以确定涡轮机性能如何以及(最重要的)为何随厚度和外倾角而变化。选择的转子叶片为NACA0012,NACA0022,NACA5522和LS0421。涡轮转子的直径为d = 3.1 m,叶片弦长为c = 0.18 m。在检查的叶尖速比范围内,NACA0012曲线在λ= 3.5时具有最高50%的整体性能。稍微弯曲的机翼(例如LS042I)可以改善垂直轴风力涡轮机的整体性能,而5%的弯曲度(NACA5522)则导致性能不佳。在测试的弧形叶片中,LS0421在λ= 3.5时的最大CP为0.40时表现最佳。沿着叶片路径的外倾会导致叶片在上风和下风区域产生更高的扭矩值。还确定了倒弯的轮廓主要在上风区域产生动力。

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